NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Enhancement of mixing in a rectangular jet by mechanical tabsThis effort was conducted to obtain additional test data/configurations required to better understand the effects of tab length and width on jet mixing enhancement for a rectangular nozzle. The configurations tested were a six-tab configuration defined by NASA, a full-height tab configuration, and two-tab configurations with selected tab lengths and widths. Additional test data were also required for all candidate configurations to better interpret the data. Test data from this effect are presented. On the basis of these data, the following general observations were noted: The six-tab rectangular nozzle configuration provided a lower peak velocity than either the two-tab or four-tab configuration; and the rectangular nozzle with a full-height tab had about the same peak velocity as the two-tab configuration; however, the full-height tab configuration had a somewhat lower centerline velocity.
Document ID
19940028366
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brown, W. H.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Ahuja, K. K.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:185207
A-8402
NASA-CR-185207
Report Number: NAS 1.26:185207
Report Number: A-8402
Report Number: NASA-CR-185207
Accession Number
94N32872
Funding Number(s)
PROJECT: RTOP 505-62-00
CONTRACT_GRANT: NAG3-1062
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available